Journal of Civil Aviation University of China ›› 2025, Vol. 43 ›› Issue (4): 36-42.

• Future airports and smart equipment • Previous Articles     Next Articles

Study on vibration characteristics of scarf patch repaired composite honeycomb
panel under hygrothermal conditions

  

  1. a. College of Transportation Science and Engineering; b. College of Aeronautical Engineering, CAUC, Tianjin 300300, China 
  • Received:2023-04-30 Revised:2023-05-21 Online:2025-09-22 Published:2025-09-22

Abstract:

Through the modal test and finite element simulation of the carbon fiber epoxy resin/Nomex paper honeycomb
panel which is one-side stepped scarf patch repaired, the vibration characteristics of the scarf patch repaired
composite honeycomb panel (abbreviated as honeycomb repaired panel) under hygrothermal conditions were
explored. Using the segmented shear deformation theory and the hygrothermal equivalent theory, a finite element
model for one-side stepped scarf patch honeycomb repaired panel was established. The effect of repairing parameters on the natural frequency of honeycomb repaired panel under different hygrothermal conditions was analyzed. The results showed that the stiffness of the composite honeycomb panels decreases due to scarf patch repairing, and the smaller the slope of scarf patch, the more the motherboard is removed, the lower the stiffness of
the honeycomb panels, and the effect is more significant under hygrothermal conditions. In the range of temperature from 300 K to 375 K and humidity from 0 to 0.75%, the natural frequency of honeycomb repaired panels decreases more significantly in hygroscopic conditions than that in thermal conditions. The combined effect of hygrothermal has a greater impact on the natural frequency reduction of honeycomb repaired panels than superposition of the separate effects of hygroscopic and thermal conditions.

Key words:

acteristic

CLC Number: